WO2007079474A2 - Directional support structure - Google Patents

Directional support structure Download PDF

Info

Publication number
WO2007079474A2
WO2007079474A2 PCT/US2007/060043 US2007060043W WO2007079474A2 WO 2007079474 A2 WO2007079474 A2 WO 2007079474A2 US 2007060043 W US2007060043 W US 2007060043W WO 2007079474 A2 WO2007079474 A2 WO 2007079474A2
Authority
WO
WIPO (PCT)
Prior art keywords
support structure
mounting plate
mounting bracket
structure according
directional support
Prior art date
Application number
PCT/US2007/060043
Other languages
French (fr)
Other versions
WO2007079474A3 (en
Inventor
Wayne Staney
Original Assignee
Wayne Staney
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wayne Staney filed Critical Wayne Staney
Publication of WO2007079474A2 publication Critical patent/WO2007079474A2/en
Publication of WO2007079474A3 publication Critical patent/WO2007079474A3/en

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/125Means for positioning
    • H01Q1/1264Adjusting different parts or elements of an aerial unit
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon Stands for scientific apparatus such as gravitational force meters
    • F16M11/02Heads
    • F16M11/04Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
    • F16M11/06Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
    • F16M11/10Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting around a horizontal axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon Stands for scientific apparatus such as gravitational force meters
    • F16M11/20Undercarriages with or without wheels
    • F16M11/2007Undercarriages with or without wheels comprising means allowing pivoting adjustment
    • F16M11/2014Undercarriages with or without wheels comprising means allowing pivoting adjustment around a vertical axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S30/00Arrangements for moving or orienting solar heat collector modules
    • F24S30/40Arrangements for moving or orienting solar heat collector modules for rotary movement
    • F24S30/42Arrangements for moving or orienting solar heat collector modules for rotary movement with only one rotation axis
    • F24S30/425Horizontal axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/40Clamping arrangements where clamping parts are received in recesses of elements to be connected
    • F16B2200/406Clamping parts being collars, bushings or wedges
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/50Flanged connections
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/50Flanged connections
    • F16B2200/503Flanged connections the flange being separate from the elements to be connected
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/50Flanged connections
    • F16B2200/506Flanged connections bolted or riveted
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S30/00Arrangements for moving or orienting solar heat collector modules
    • F24S2030/10Special components
    • F24S2030/13Transmissions
    • F24S2030/135Transmissions in the form of threaded elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S25/00Arrangement of stationary mountings or supports for solar heat collector modules
    • F24S25/10Arrangement of stationary mountings or supports for solar heat collector modules extending in directions away from a supporting surface
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/40Solar thermal energy, e.g. solar towers
    • Y02E10/47Mountings or tracking

Definitions

  • the present invention relates to field of support structures and, more particularly, to a support structure for solar panel collectors, satellite antennas and other objects that need to be fixed toward a point in space.
  • Solar panels and satellite antennas are directed to a particular point in space to be effective.
  • a solar panel collector must either be directed toward the sun where it will be most effective or made to track the sun as it moves across the sky.
  • Solar panels are used to collect energy from the Sun and require optimum positioning whether the energy is for heating of water or providing electrical power. The weight of the panels is dependant upon the panel size but can be quite heavy if the solar panel includes circulating water.
  • Satellite antennas both flat and parabolic, can be found throughout the world for communication purposes. These antennas must also be directed to a particular point in space to be effective. Solar panels and satellite antennas both require support structures capable of adjustment yet capable of inhibiting all movement even if presented with high winds.
  • the directional support structure includes an adjustable bracket that allows for pivoting of the mounting plate even when the mounting plate is loaded with solar panels or satellite panels, despite the weight of such devices. Rotational or azimuth movement is maintained by use of a mounting bracket secured to a base member that allows rotation with operator safety in mind by eliminating disengagement of the directional devices once they are secured to the mounting plate. Upon proper rotational placement, flanges are fastened together sandwiching a flaring located on the lower end of the mounting bracket thereby preventing further rotational movement.
  • ⁇ base member includes a hollow column that can be placed in the ground or bolted on a fixed structure.
  • the column is hollow to provide a wire chase for concealment of pipes and/or electrical wiring.
  • Still another objective of the instant invention is to disclose .the use of a universal mounting plate capable of holding a plurality of solar panel basins.
  • Still another objective of the instant invention is to disclose the use of solar panel basins that allow for the flush mount of solar panels to protect from side wind lifting.
  • Still another objective of the instant invention is to teach the use of a mounting plate that can be used for most any device that requires directional placement including use of satellite antenna panel.
  • Figure 1 is a side plane view of the Directional Support Structure
  • Figure Ia is a pictorial of Figure 1.
  • Figure 2 is an exploded view illustrating a flaring attached to a lower end of the mounting bracket
  • Figure 2a is an exploded view illustrating a flaring attached to the upper end of the base member;
  • Figure 3 illustrates a front perspective view of the Directional Support Structure within an attached basin for receipt of solar panels;
  • Figure 3a is a pictorial of Figure 3;
  • Figure 4 is a side perspective of the Directional
  • Figure 4a is a pictorial of Figure 4.
  • Figure 5 is a side perspective view of the Directional Support Structure with a satellite antenna and collector.
  • FIG. 1 set forth is a side view of the directional support structure 10 which consists of a mounting plate 12 having a front surface 14 and a rear surface 16.
  • the mounting plate includes mounting apertures, not shown, that can be pre drilled or the mounting plate can be modified for receipt of solar panels, antennas, solar panel basins, and the like type objects that need directional positioning toward a point in space.
  • the mounting plate 12 is coupled to an extension tube 18 having a proximal end 20 secured to the rear surface 16 with a mounting plate. Securement of the extension tube 18 to the mounting plate 12 is preferably be a weldment providing structural strength for carrying of heavy objects.
  • the extension tube maintaining rigidity from heavy loads such as snow, or high winds such as hurricanes.
  • the extension tube 18 is preferably mounted perpendicular to the mounting plate and extending outwardly to a distal end 22 placed at a position that allows for proper pivoting as explained herein.
  • the extension tube 18 is pivotally mounted to a mounting bracket 24 by pivot point 26.
  • the pivot point is a fastener that extends from one side of the extension tube to the opposite side and coupling to a first mounting bracket 24 which may be of a single side or preferably includes a second bracket forming a mirror image of the first mounting bracket.
  • the mounting bracket 24 is positioned on each side of the extension tube with the mounting fastener 26 extending through the extension tube and is tightened to prevent lateral movement of the extension tube but maintain pivoting by adjustment of turn buckle coupling 28.
  • the mounting bracket 24 permits latitude alignment of the mounting plate 12 by pivoting of the extension tube 18 along pivot point fastener 26.
  • a second end 30 of the mounting bracket is secured to base member 32.
  • the base member 32 is formed from a hollow upright column 34 defined by an upper end 36 spaced apart from a lower end 38 a distance to allow clearance of the mounting plate 12 from contacting an object when a solar panel or antenna is placed thereon.
  • the base member 32 is coupled to the mounting bracket 24 by use of flanges and a flare.
  • a flare 40 is mounted to the bottom 30 of the mounting bracket with a movable flange 42 positioned on said mounting bracket and available for attachment to a cooperating second flange 44 located on the upper end of the base member 32.
  • the first flange 42 includes fasteners 46 which are preferably threaded bolts for insertion in engagement with threaded apertures 48 located on the second flange 44. During installation the first flange is loosely coupled to the second flange sandwiching the flaring 40 there between.
  • the mounting bracket 24 can be rotated as necessary for directional alignment of the device to be pointed toward a point in space and upon proper alignment the first flange 42 is securely fastened to the second flange 44 by placement of threaded bolts 46 tightly into apertures 48 thereby sandwiching the flare in 40 there between.
  • the first flange 42 includes a receptacle 50 sized to cooperated with the flare 40 thereby capturing the flare in a fixed position.
  • the first flange 42 ' is permanently secured to the mounting bracket 24 ' wherein flare 40' is permanently attached to base member 32'.
  • a second flange 44 ' is coupled to the first flange 42 sandwiching the flare 40" there between. Similar to the first embodiment the use of fasteners 46 engage threaded apertures 48' to cause a tight sandwich between the first and second flange fixing the flaring in between.
  • second flange 44' may include a receptacle 50* sized to receive the flare 40'.
  • the turn buckle 28 is adjustable having a left hand thread 60 and a right hand thread 62.
  • the extension tube 18 can be tilted by causing the distal end 22 to be narrowed or spaced apart from the mounting bracket lower end 30.
  • the turn buckle is pivotally coupled to the extension tube by fastener 66 into the mounting bracket by fastener 68.
  • a locking nut 70 can be tightened against the body of the turn buckle 64 to prevent movement.
  • a second turn buckle forms a mirror image of the first turn buckle.
  • left hand and right hand threads could be reversed and other devices may be employed for the purpose of extending or diminishing the distance between end 30 and the distal end 22 of the extension tube for purposes of causing latitude tilting of the mounting plate 12.
  • FIG. 3 is a front perspective view of the directional support structure 10 depicting the base member 32 having a lower flange 38 secured to a rigid structure, not shown, by fasteners 39.
  • the upper end of the base member having secured to mounting bracket 24 by first flange 42 fastened to second flange 44 by fasteners 46.
  • the mounting bracket is pivotally secured to the mounting plate 12 by the pivotal coupling 26 and adjusted by use of turn buckles 28 and 28'.
  • the use of turn buckles on each side of the mounting bracket 24 provides rigidity by using the extension tube 18 which is preferably a square or rectangular rigid material providing absolute rigidity.
  • the use of a solar collector basin 102 is illustrated.
  • the solar basin includes recessed cavities 104 and 106 that allow placement of the panels into the basin allowing the solar panels to remain flush to prevent loading of the panels by wind or other elements that would other wise structurally effect the strength and efficiency of the solar panels.
  • Figure 4 depicts the solar panels 108 placed in receptacle 104 and panel 110 place in receptacle 106. It should be noted that a single receptacle or multiple receptacles may be employed depending upon the type of solar panel utilized.
  • FIG. 5 set forth is an illustrated example of an alternative embodiment for use with the directional support structure 10 wherein a flat antenna device 120 is employed having a signal collector 122 positioned over the satellite panel 120 for signal reception.
  • Flat panels are known in the art as being by the instant inventor such as that set forth in U.S. Patent No. 5,512,913 being a flat plate antenna, the contents of which are incorporated herein in by reference.

Abstract

A directional support structure for use with solar panels, flat satellite antennas, and the like items that are directed toward a point in space. The support structure has a mounting plate with an extension tube extending outwardly therefrom and is pivotally secured to a mounting bracket permitting latitude alignment of the mounting plate. At least one adjustable turnbuckle is attached to the extension tube and the mounting bracket to provide adjustable alignment of the mounting plate, the turnbuckle can then be locked into position. The mounting bracket is further secured to a base member permitting rotational or azimuth positioning of the mounting plate. The base member includes an attached first flange positioned along an upper end of the base member, an attached flaring positioned to the lower end of the mounting bracket, and an unattached second flange positioned over the flaring and securable to the first flange with fasteners. The support structure can be loosely assembled with industrial solar panels or antennas yet is effortless to position for optimum directional positioning. The mounting bracket may then be rotationally positioned and the flanges fastened together to lock the mounting bracket in a fixed position.

Description

DIRECTIONAL SUPPORT STRUCTURE
FIELD OF THE INVENTION
The present invention relates to field of support structures and, more particularly, to a support structure for solar panel collectors, satellite antennas and other objects that need to be fixed toward a point in space.
BACKGROUND INFORMATION Solar panels and satellite antennas are directed to a particular point in space to be effective. A solar panel collector must either be directed toward the sun where it will be most effective or made to track the sun as it moves across the sky. Solar panels are used to collect energy from the Sun and require optimum positioning whether the energy is for heating of water or providing electrical power. The weight of the panels is dependant upon the panel size but can be quite heavy if the solar panel includes circulating water.
Satellite antennas, both flat and parabolic, can be found throughout the world for communication purposes. These antennas must also be directed to a particular point in space to be effective. Solar panels and satellite antennas both require support structures capable of adjustment yet capable of inhibiting all movement even if presented with high winds.
One of the problems with the prior art support structures is the inability to precisely hold large directional objects yet allow for ease of adjustment. For instance, if a solar panel is designed to be fixed, as opposed to a tracking panel, the necessity for the safety of the installers is paramount as conventional support structures place a burden upon the installer to prevent damage during directional positioning. In addition, prior art devices have not disclosed the necessity for a support structure capable of withstanding extremely high winds such as hurricanes which can cause misadjustment should the panel move even one inch.
Thus, what is lacking in the art is a heavy duty directional support structure capable of holding large heavy panels yet provide ease in directionalIy pointing by allowing the installer to rotate and tilt the directional panel as necessary.
SUMMARY OF THE INVENTION Set forth is a directional support structure for use with solar panels, flat or raised satellite antennas, and the like structures required to be directionally facing a fixed point in space. The directional support structure includes an adjustable bracket that allows for pivoting of the mounting plate even when the mounting plate is loaded with solar panels or satellite panels, despite the weight of such devices. Rotational or azimuth movement is maintained by use of a mounting bracket secured to a base member that allows rotation with operator safety in mind by eliminating disengagement of the directional devices once they are secured to the mounting plate. Upon proper rotational placement, flanges are fastened together sandwiching a flaring located on the lower end of the mounting bracket thereby preventing further rotational movement. An adjustment bracket is provided to allow latitude adjustment of the mounting plate by use of turn buckles that provide precise adjustment and absolute rigidity upon locking of the turn buckles . Α base member includes a hollow column that can be placed in the ground or bolted on a fixed structure. ■ The column is hollow to provide a wire chase for concealment of pipes and/or electrical wiring.
Thus, an objective of the instant invention is to disclose a directional support structure capable of azimuth and latitude adjustment despite the weight of the devices to be directionally positioned. Yet another objective of the invention is to provide a support structure that provides a safe structure for installers by creating a rigid mounting base that allows ■for positional adjustment. Still another objective of the instant invention is to provide an industrial stand capable of withstanding weather with standing extremities such as hurricane winds without movement of the positioning elements.
Still another objective of the instant invention is to disclose .the use of a universal mounting plate capable of holding a plurality of solar panel basins.
Still another objective of the instant invention is to disclose the use of solar panel basins that allow for the flush mount of solar panels to protect from side wind lifting.
Still another objective of the instant invention is to teach the use of a mounting plate that can be used for most any device that requires directional placement including use of satellite antenna panel. The above-stated objectives as well as other objectives which, although not specifically stated, are intended to be included within the scope of the present invention, are accomplished by the present invention and will become apparent from the hereinafter set forth Detailed Description of the Invention, Drawings, and the Claims appended herewith.
BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1 is a side plane view of the Directional Support Structure; Figure Ia is a pictorial of Figure 1.;
Figure 2 is an exploded view illustrating a flaring attached to a lower end of the mounting bracket;
Figure 2a is an exploded view illustrating a flaring attached to the upper end of the base member; Figure 3 illustrates a front perspective view of the Directional Support Structure within an attached basin for receipt of solar panels;
Figure 3a is a pictorial of Figure 3; Figure 4 is a side perspective of the Directional
Support Structure with solar panels placed in a basin;
Figure 4a is a pictorial of Figure 4; and
Figure 5 is a side perspective view of the Directional Support Structure with a satellite antenna and collector.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
As required, detailed embodiments of the present invention are disclosed herein; however, it is to be understood that the disclosed embodiments are merely exemplary of the invention which may be embodied in various forms. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the present invention in virtually any appropriately detailed structure.
Referring now to Figures 1 and Ia, set forth is a side view of the directional support structure 10 which consists of a mounting plate 12 having a front surface 14 and a rear surface 16. The mounting plate includes mounting apertures, not shown, that can be pre drilled or the mounting plate can be modified for receipt of solar panels, antennas, solar panel basins, and the like type objects that need directional positioning toward a point in space. The mounting plate 12 is coupled to an extension tube 18 having a proximal end 20 secured to the rear surface 16 with a mounting plate. Securement of the extension tube 18 to the mounting plate 12 is preferably be a weldment providing structural strength for carrying of heavy objects. The extension tube maintaining rigidity from heavy loads such as snow, or high winds such as hurricanes. The extension tube 18 is preferably mounted perpendicular to the mounting plate and extending outwardly to a distal end 22 placed at a position that allows for proper pivoting as explained herein. The extension tube 18 is pivotally mounted to a mounting bracket 24 by pivot point 26. Preferably the pivot point is a fastener that extends from one side of the extension tube to the opposite side and coupling to a first mounting bracket 24 which may be of a single side or preferably includes a second bracket forming a mirror image of the first mounting bracket. In this manner the mounting bracket 24 is positioned on each side of the extension tube with the mounting fastener 26 extending through the extension tube and is tightened to prevent lateral movement of the extension tube but maintain pivoting by adjustment of turn buckle coupling 28. The mounting bracket 24 permits latitude alignment of the mounting plate 12 by pivoting of the extension tube 18 along pivot point fastener 26. A second end 30 of the mounting bracket is secured to base member 32. The base member 32 is formed from a hollow upright column 34 defined by an upper end 36 spaced apart from a lower end 38 a distance to allow clearance of the mounting plate 12 from contacting an object when a solar panel or antenna is placed thereon. This is particularly helpful when the base member is mounted on the ground wherein the mounting plate extends up over the ground a distance which will handle most average snow falls, and allows shrubbery or other lawn items to be placed around the base without interfering with the solar panel and or satellite antenna reception- Referring now to Figure 2 the base member 32 is coupled to the mounting bracket 24 by use of flanges and a flare. In a preferred embodiment a flare 40 is mounted to the bottom 30 of the mounting bracket with a movable flange 42 positioned on said mounting bracket and available for attachment to a cooperating second flange 44 located on the upper end of the base member 32. The first flange 42 includes fasteners 46 which are preferably threaded bolts for insertion in engagement with threaded apertures 48 located on the second flange 44. During installation the first flange is loosely coupled to the second flange sandwiching the flaring 40 there between. The mounting bracket 24 can be rotated as necessary for directional alignment of the device to be pointed toward a point in space and upon proper alignment the first flange 42 is securely fastened to the second flange 44 by placement of threaded bolts 46 tightly into apertures 48 thereby sandwiching the flare in 40 there between.
In a preferred embodiment the first flange 42 includes a receptacle 50 sized to cooperated with the flare 40 thereby capturing the flare in a fixed position. Alternatively, referring to Figure 2a, the first flange 42 ' is permanently secured to the mounting bracket 24 ' wherein flare 40' is permanently attached to base member 32'. In this embodiment a second flange 44 ' is coupled to the first flange 42 sandwiching the flare 40" there between. Similar to the first embodiment the use of fasteners 46 engage threaded apertures 48' to cause a tight sandwich between the first and second flange fixing the flaring in between. Similarly in the second embodiment second flange 44' may include a receptacle 50* sized to receive the flare 40'. Again referring Figure 1 the turn buckle 28 is adjustable having a left hand thread 60 and a right hand thread 62. By rotation of the turn buckle body 64 the extension tube 18 can be tilted by causing the distal end 22 to be narrowed or spaced apart from the mounting bracket lower end 30. The turn buckle is pivotally coupled to the extension tube by fastener 66 into the mounting bracket by fastener 68. When the turn buckle is rotated to present the proper latitude alignment of the mounting plate 12 a locking nut 70 can be tightened against the body of the turn buckle 64 to prevent movement. For ease of simplicity, only a single turn buckle is described. A second turn buckle forms a mirror image of the first turn buckle. In addition, it should be noted that the left hand and right hand threads could be reversed and other devices may be employed for the purpose of extending or diminishing the distance between end 30 and the distal end 22 of the extension tube for purposes of causing latitude tilting of the mounting plate 12.
Now referring to Figure 3 set forth, is a front perspective view of the directional support structure 10 depicting the base member 32 having a lower flange 38 secured to a rigid structure, not shown, by fasteners 39. The upper end of the base member having secured to mounting bracket 24 by first flange 42 fastened to second flange 44 by fasteners 46. The mounting bracket is pivotally secured to the mounting plate 12 by the pivotal coupling 26 and adjusted by use of turn buckles 28 and 28'. In the preferred embodiment the use of turn buckles on each side of the mounting bracket 24 provides rigidity by using the extension tube 18 which is preferably a square or rectangular rigid material providing absolute rigidity. In this embodiment the use of a solar collector basin 102 is illustrated. The solar basin includes recessed cavities 104 and 106 that allow placement of the panels into the basin allowing the solar panels to remain flush to prevent loading of the panels by wind or other elements that would other wise structurally effect the strength and efficiency of the solar panels. Figure 4 depicts the solar panels 108 placed in receptacle 104 and panel 110 place in receptacle 106. It should be noted that a single receptacle or multiple receptacles may be employed depending upon the type of solar panel utilized.
Referring to Figure 5 set forth is an illustrated example of an alternative embodiment for use with the directional support structure 10 wherein a flat antenna device 120 is employed having a signal collector 122 positioned over the satellite panel 120 for signal reception. Flat panels are known in the art as being by the instant inventor such as that set forth in U.S. Patent No. 5,512,913 being a flat plate antenna, the contents of which are incorporated herein in by reference.
It should be understood that the foregoing relates to only preferred embodiments of the present invention, and that it is intended to cover all changes and modifications of the embodiment of the invention herein used for the purposes of disclosure, which do not institute departures from the spirit and scope of the invention.

Claims

Claims What is claimed is:
Claim 1. A directional support structure comprising: a mounting plate having a front surface and a rear surface; an extension tube having a proximal end secured to said rear surface with a distal end extending outwardly therefrom and perpendicular thereto; a mounting bracket having a first end pivotally secured to said extension tube permitting latitude alignment of said mounting plate, and a second end secured to a base member permitting rotational positioning of said mounting plate, said base member formed from an upright column defined by a upper end spaced apart from a lower end; and at least one adjustable tie rod coupling said extension tube said mounting bracket, said tie rod coupling fixating said latitude alignment of said mounting plate; whereby items placed on said front surface of said mounting plate can be optimally positioned to face a point in space by rotatably adjusting said mounting bracket and by pivotedly adjusting said extension tube.
Claim 2. The directional support structure according to Claim 1 including an attached first flange positioned to said upper end of said base member, an attached flaring positioned to said lower end of said mounting bracket, and an unattached second flange positioned over said flaring and securable to said first flange with fasteners, wherein said mounting bracket may be rotationally positioned and said flanges fastened together to lock said mounting bracket in a fixed position.
Claim 3. The directional support structure according to Claim 1 wherein said tie rod is further defined as a variable length turnbuckle having left hand and right hand treads for securing said latitude alignment of said mounting plate.
Claim 4. The directional support structure according to Claim 3 wherein said turnbuckle is includes a locking nut.
Claim 5. The directional support structure according to Claim 1 wherein said upright column is hollow.
Claim 6. The directional support structure according to Claim 1 wherein said lower end of said base member is inserted into the ground.
Claim 7. The directional support structure according to Claim 1 including an anchor flange secured to the bottom of said vertical column, said anchor flange available for attachment to a rigid foundation by use of fasteners.
Claim 8. The directional support structure according to Claim 2 wherein said flaring is attached to said upper end of said base member and said unattached second flange is positioned beneath said flaring and securable to said first flange with fasteners, wherein said mounting bracket may be rotationally positioned and said flanges fastened together to lock said mounting bracket in a fixed position.
Claim 9. The directional support structure according to Claim 1 including an offset boss for coupling to one end of said tie rod.
Claim 10. The directional support structure according to Claim 1 including a tub basin securable to said mounting plate, said tub basin recessed and receptive to the placement of at least one flush mounted solar panel.
Claim 11. The directional support structure according to Claim 10 wherein said tub basin includes at least one divider for receipt of additional solar panels.
Claim 12. The directional support structure according to Claim 1 wherein said mounting plate is receptive to a flat satellite panel antenna.
Claim 13. The directional support structure according to Claim 12 including a signal collector coupled to opposite edges of said mounting plate and bridging across said flat satellite panel antenna.
Claim 14. A directional support structure comprising: a mounting plate having a front surface and a rear surface; an extension tube having a proximal end secured to said rear surface with a distal end extending outwardly therefrom and perpendicular thereto; a mounting bracket having a first end pivotally secured to said extension tube permitting latitude alignment of said mounting plate, and a second end secured to a base member permitting rotational positioning of said mounting plate, said base member formed from a hollow upright column defined by a upper end spaced apart from a lower end, said base member having an attached first flange positioned to said upper end of said base member, an attached flaring positioned to said lower end of said mounting bracket, and an unattached second flange positioned over said flaring and securable to said first flange with fasteners, wherein said mounting bracket may be rotationally positioned and said flanges fastened together to lock said mounting bracket in a fixed position; and at least one adjustable turnbuckle coupling said extension tube said mounting bracket, said tie rod coupling fixating said latitude alignment of said mounting plate; whereby items placed on said front surface of said mounting plate can be optimally positioned to face a point in space by rotatably adjusting said mounting bracket and by pivotedly adjusting said extension tube.
Claim 15. The directional support structure according to Claim 14 wherein said turnbuckle includes left hand and right hand treads for securing said latitude alignment of said mounting plate.
Claim 16. The directional support structure according to Claim 15 wherein said turnbuckle is includes a locking nut.
Claim 17. The directional support structure according to Claim 14 wherein said hollow column includes a wire chase.
Claim 18. The directional support structure according to Claim 14 wherein said lower end of said base member is inserted into the ground.
Claim 19. The directional support structure according to Claim 14 including an anchor flange secured to the bottom of said vertical column, said anchor flange available for attachment to a rigid foundation by use of fasteners.
Claim 20. The directional support structure according to Claim 14 wherein said flaring is attached to said upper end of said base member and said unattached second flange is positioned beneath said flaring and securable to said first flange with fasteners, wherein said mounting bracket may be rotationally positioned and said flanges fastened together to lock said mounting bracket in a fixed position.
Claim 21. The directional support structure according to Claim 14 including a tub basin securable to said mounting plate, said tub basin recessed and receptive to the placement of at least one flush mounted solar panel.
Claim 22. The directional support structure according to Claim 14 wherein said mounting plate is receptive to a flat satellite panel antenna.
Claim 23. The directional support structure according to Claim 14 including a signal collector coupled to opposite edges of said mounting plate and bridging across said flat satellite panel antenna.
PCT/US2007/060043 2006-01-04 2007-01-03 Directional support structure WO2007079474A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/326,589 2006-01-04
US11/326,589 US7374137B2 (en) 2006-01-04 2006-01-04 Directional support structure

Publications (2)

Publication Number Publication Date
WO2007079474A2 true WO2007079474A2 (en) 2007-07-12
WO2007079474A3 WO2007079474A3 (en) 2008-10-09

Family

ID=38223404

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2007/060043 WO2007079474A2 (en) 2006-01-04 2007-01-03 Directional support structure

Country Status (2)

Country Link
US (1) US7374137B2 (en)
WO (1) WO2007079474A2 (en)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CZ13495U1 (en) * 2003-05-16 2003-07-14 Pavel Truksa Device for fixation of position of collapsible modular systems
DE102007011620B4 (en) * 2007-01-22 2012-11-08 Airbus Operations Gmbh Lining scaffolding for a plane
ES2326204B1 (en) * 2007-10-24 2010-05-26 Talleres Clavijo S.L. IMPROVEMENTS IN THE ORIENTABLE SOLAR PANEL SYSTEMS.
IT1391223B1 (en) * 2008-09-23 2011-12-01 Altertecno S R L Ora Altertecno S N C Di Carlo Avoni STRUCTURE WITH ADJUSTABLE SOLAR PANELS.
BRPI0922669B1 (en) * 2008-12-15 2020-11-10 Sea Tel, Inc.(D/B/A Cobham Satcom Marine Systems) pedestal for a tracking antenna
US7871031B2 (en) * 2009-03-23 2011-01-18 Tekpak Corporation Device having a liftable strap supply reel
US8423201B2 (en) * 2009-05-13 2013-04-16 United States Antenna Products, LLC Enhanced azimuth antenna control
WO2011024084A2 (en) * 2009-08-26 2011-03-03 Hunt Robert D Solar thermal energy concentrating building material
US20100139741A1 (en) * 2009-10-12 2010-06-10 Wares Brian S Frame-Integrated Pivot Bearing For Solar Collector Assembly
US9462734B2 (en) 2010-04-27 2016-10-04 Alion Energy, Inc. Rail systems and methods for installation and operation of photovoltaic arrays
US20110266411A1 (en) * 2010-04-29 2011-11-03 David Silverberg Ergonomically balanced and moveable arm support system
US9343592B2 (en) 2010-08-03 2016-05-17 Alion Energy, Inc. Electrical interconnects for photovoltaic modules and methods thereof
US8779278B2 (en) 2010-09-23 2014-07-15 Raytheon Company Air supported photovoltaic system
TWI449260B (en) * 2011-02-23 2014-08-11 Wistron Neweb Corp Adjusting mechanism for adjusting rotation angle and antenna system therewith
US9746207B1 (en) * 2011-03-16 2017-08-29 Solarreserve Technology, Llc Tracking modules including tip/tilt adjustability and construction features
US9641123B2 (en) * 2011-03-18 2017-05-02 Alion Energy, Inc. Systems for mounting photovoltaic modules
US8866695B2 (en) * 2012-02-23 2014-10-21 Andrew Llc Alignment stable adjustable antenna mount
US9352941B2 (en) 2012-03-20 2016-05-31 Alion Energy, Inc. Gantry crane vehicles and methods for photovoltaic arrays
US8919961B2 (en) * 2012-04-30 2014-12-30 Nelson Planting Inflatable, pressure-controlled, portable line-concentrating heliostat
WO2013173178A1 (en) 2012-05-16 2013-11-21 Alion, Inc. Rotatable support systems for photovoltaic modules and methods thereof
US9551508B2 (en) * 2013-06-24 2017-01-24 James E. Straeter Ground mounted solar power assembly
AU2014315407B2 (en) 2013-09-05 2018-12-13 Alion Energy, Inc. Systems, vehicles, and methods for maintaining rail-based arrays of photovoltaic modules
US9453660B2 (en) 2013-09-11 2016-09-27 Alion Energy, Inc. Vehicles and methods for magnetically managing legs of rail-based photovoltaic modules during installation
CN103637660B (en) * 2013-12-04 2016-03-30 昆明理工大学 A kind of Multifunctional hanging rack
US9255725B2 (en) * 2014-01-30 2016-02-09 Jasem M K Th Sh Al-Enizi Sun tracking solar energy collection system
US10077921B2 (en) * 2014-10-14 2018-09-18 Eduardo Saucedo Re-reflecting paraboloid dish collector
US9553350B2 (en) 2015-05-14 2017-01-24 Micro Wireless Solutions, Corp. Antenna mount assembly
WO2017044566A1 (en) 2015-09-11 2017-03-16 Alion Energy, Inc. Wind screens for photovoltaic arrays and methods thereof
CN107344459A (en) * 2016-05-06 2017-11-14 力山工业股份有限公司 Multi-functional microscope carrier
JP6893688B2 (en) * 2017-06-20 2021-06-23 株式会社ナチュラレーザ・ワン Switchgear switchgear and various switchgear equipped with this switchgear switchgear
EP4224627A1 (en) * 2018-03-08 2023-08-09 ViaSat Inc. Antenna positioner with eccentric tilt position mechanism
CN112204430A (en) * 2018-07-13 2021-01-08 株式会社久保田 Working machine and positioning system for working machine
US11666143B2 (en) * 2019-05-14 2023-06-06 Fellowes Inc. Multi-positional articulating ergonomic device with modular features
US11575195B2 (en) * 2019-12-04 2023-02-07 Commscope Technologies Llc Mechanical tilt mounting system for a base station antenna
US11038253B1 (en) * 2020-03-18 2021-06-15 Jonsa Technologies Co., Ltd. Satellite antenna azimuth adjustment assembly
ES2854474B2 (en) * 2020-03-20 2022-06-21 Esasolar Energy System S L SOLAR TRACKER WITH LOCKING SYSTEM
US11108353B1 (en) 2020-07-14 2021-08-31 FTC Solar, Inc. Systems and methods for array level terrain based backtracking
US11139775B1 (en) 2020-07-14 2021-10-05 FTC Solar, Inc. Systems and methods for terrain based backtracking for solar trackers
US11522491B2 (en) 2020-08-26 2022-12-06 FTC Solar, Inc. Systems and methods for adaptive range of motion for solar trackers
US10935992B1 (en) 2020-09-16 2021-03-02 FTC Solar, Inc. Systems and methods for solar trackers with diffuse light tracking

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4126865A (en) * 1975-11-11 1978-11-21 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Satellite tracking dish antenna
US4138991A (en) * 1976-07-31 1979-02-13 Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft-Man Flat solar collector
US4819006A (en) * 1986-05-08 1989-04-04 Aluminum Company Of America Mount for supporting a parabolic antenna
US6037913A (en) * 1999-05-13 2000-03-14 Johnson; Pamela Kay Moveable satellite dish antenna mount
US6195066B1 (en) * 1999-01-19 2001-02-27 Thomas C. Pegues, Jr. Satellite dish mounting arm

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3593954A (en) * 1970-06-04 1971-07-20 Kofabco Inc Swivel connection for a chair
US3714660A (en) 1970-07-23 1973-01-30 Itt Antenna mounting structure
US3940771A (en) 1975-04-21 1976-02-24 Rockwell International Corporation Variable angle support apparatus
US4232320A (en) 1978-04-21 1980-11-04 Andrew Corporation Mount for earth station antenna
US4251819A (en) 1978-07-24 1981-02-17 Ford Aerospace & Communications Corp. Variable support apparatus
US4300537A (en) 1980-09-19 1981-11-17 Davis Thomas A Solar panel mount
US4545557A (en) 1983-07-22 1985-10-08 Rogers Bernard J D Articulated mounting means for poles, antennas and the like
US4617572A (en) * 1984-08-14 1986-10-14 Albert Hugo Television dish antenna mounting structure
US4783662A (en) 1986-02-18 1988-11-08 Delta Satellite Corportion Polar mount for satellite dish antenna
JPS62256503A (en) * 1986-04-30 1987-11-09 Tsubakimoto Chain Co Turning drive equipment for parabolic antenna
GB8615400D0 (en) * 1986-06-24 1986-07-30 Isc Chemicals Ltd Flourinated polycyclic compounds
US4799642A (en) 1987-02-03 1989-01-24 Rt/Katek Communications Group, Inc. Antenna mounting
US4819007A (en) * 1987-06-22 1989-04-04 Andrew Corporation Supporting structure for reflector-type microwave antennas
US4918363A (en) * 1988-09-30 1990-04-17 Venture Mfg. Co. Actuator for TVRO parabolic antenna
US5007560A (en) * 1989-03-01 1991-04-16 Sassak John J Beer dispensing and monitoring method and apparatus
US4922264B1 (en) 1989-04-24 1995-11-21 Robert M Fitzgerald Satellite antenna mounting apparatus with ballast means
US5075682A (en) * 1990-03-30 1991-12-24 Dehnert Douglas K Antenna mount and method for tracking a satellite moving in an inclined orbit
US5512913A (en) * 1992-07-15 1996-04-30 Staney; Michael W. Flat plate antenna, scaler collector and supporting structure
US5355145A (en) * 1992-07-30 1994-10-11 Lucas Donald E Satellite dish actuator mounting construction
US5798517A (en) * 1994-05-19 1998-08-25 Berger; Alexander Sun tracker system for a solar assembly
US5614918A (en) 1994-06-21 1997-03-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Global positioning system antenna fixed height tripod adapter
US5576722A (en) * 1994-09-13 1996-11-19 The United States Of America As Represented By The Secretary Of The Army Mobile satellite antenna base and alignment apparatus
US6284968B1 (en) 2000-06-19 2001-09-04 Joseph Z. Niesyn Solar-tracking system
US7298342B2 (en) * 2004-10-28 2007-11-20 Seaspace Corporation Antenna positioner system
US20070095993A1 (en) * 2005-10-28 2007-05-03 Fumoto Giken Co., Ltd. Moving apparatus

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4126865A (en) * 1975-11-11 1978-11-21 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Satellite tracking dish antenna
US4138991A (en) * 1976-07-31 1979-02-13 Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft-Man Flat solar collector
US4819006A (en) * 1986-05-08 1989-04-04 Aluminum Company Of America Mount for supporting a parabolic antenna
US6195066B1 (en) * 1999-01-19 2001-02-27 Thomas C. Pegues, Jr. Satellite dish mounting arm
US6037913A (en) * 1999-05-13 2000-03-14 Johnson; Pamela Kay Moveable satellite dish antenna mount

Also Published As

Publication number Publication date
WO2007079474A3 (en) 2008-10-09
US7374137B2 (en) 2008-05-20
US20070152124A1 (en) 2007-07-05

Similar Documents

Publication Publication Date Title
US7374137B2 (en) Directional support structure
US9127475B2 (en) Adjustable mount and umbrella
US8505863B2 (en) Camming clamp for roof seam
US5963179A (en) Variable azimuth mounting assembly for panel antennas
US8780008B2 (en) Reinforced mount for an antenna assembly
US7659865B2 (en) Adjustable fast set antenna frame
US4723128A (en) Roof mount for dish antenna
US7946306B2 (en) Portable garage
US20110240006A1 (en) Solar Tracking System and Method
US8698692B2 (en) Apparatus for mounting an object to a railing
WO2008088311A2 (en) Solar panel mounting apparatus with a plurality of independtently adjustable arms and rotatable vertical axis
US5142293A (en) Skylight roof mount for satellite antennas
US20110005512A1 (en) Adjustable solar panel support structure
US9010715B2 (en) Mast
US6709184B1 (en) Apparatus for mounting a receiver mast and associated method
KR101170516B1 (en) Device for manually controlling slope of solar cell module
CA2011328C (en) Support downtilt bracket for mounting an antenna on a metallic tower
US10627043B2 (en) Hinged magnetic mounting apparatus
US20070273598A1 (en) Luneberg Lens Antenna Device
US20170288603A1 (en) Solar panel self-storing adjustable angle mount
WO2017059484A1 (en) Solar reflector mount
WO2017155978A1 (en) Support assembly for photovoltaic modules and mounting system using the same
US20110121143A1 (en) Tracking system
JP2020105899A (en) Other-body fixture and installation structure of other-body fixture
CN220570489U (en) Photovoltaic support with adjustable angle

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application
NENP Non-entry into the national phase

Ref country code: DE

32PN Ep: public notification in the ep bulletin as address of the adressee cannot be established

Free format text: NOTING OF LOSS OF RIGHTS PURSUANT TO RULE 112(1) EPC, AS PER OUR COMMUNICATION DATED 5.9.2008 (EPO FORM 1205A)

122 Ep: pct application non-entry in european phase

Ref document number: 07717242

Country of ref document: EP

Kind code of ref document: A2